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Development of a Novel Helmet Support Assembly for NASA Orion Crew Survival SuitOrion Spacecraft water landing environments have necessitated the design and testing of a novel Helmet Support Assembly (HSA) as part of the NASA Orion Crew Survival Systems (OCSS) launch and re-entry spacesuit. A series of development sled tests using 5 th female, 50th male, and 95th male Hybrid III Anthropometric Test Devices (ATDs) simulated worst case water landings and identified the need for an integrated suit countermeasure to control the helmet during dynamic loading. Initial prototype countermeasures rigidly restrained the helmet keeping the helmet in place as desired, but led to large force and moment transmission to the upper neck. Further development led to a flexible HSA which used high-strength steel wire contoured to the size-matched ATD thorax and attached to both the front and rear of the neck ring. The selected wire diameter and contoured shape provided some ability to flex under the expected worst-case dynamic loads. The existing shoulder harness was used to restrain the helmet motion during “eyeballs out/down” loading while also attempting to prevent head-to-helmet contact in “eyeballs down” spinal-axis loading. A new small prototype helmet was also developed and tested for the 5th and 50th ATDs with both HSA devices. Dynamic impact tests were conducted on the HIA (Horizontal Impulse Accelerator) at Wright Patterson Air Force Base (WPAFB) under simulated off-nominal landing conditions using a representative Orion seat and 5-point harness. For each ATD size, peak Neck Injury Criteria (Nij) were compared to equivalent sled tests with an unsuited ATD configuration. Adding a helmet without attempting to control motion increased peak Nij values for all ATD sizes. The use of the rigid countermeasure showed decreased peak Nij results for the 5th female, but increased peak Nij values for both 50th configurations and the 95th male ATDs. By comparison, the flexible HSA showed reduced peak Nij values for all ATD sizes. Overall, this series of dynamic impact tests identified a risk of increased crew neck loading when under- or over-restraining the helmet during simulated Orion water landings and also demonstrated an effective strategy to mitigate those loads with a compliant HSA design.
Document ID
20200001579
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Suhey, Jeffrey
(NASA Johnson Space Center Houston, TX, United States)
Gohmert, Dustin
(NASA Johnson Space Center Houston, TX, United States)
Jacobs, Shane
(Clark (David) Co., Inc. Worcester, MA, United States)
Baldwin, Mark A.
(Lockheed Martin Corp. Houston, TX, United States)
Date Acquired
March 13, 2020
Publication Date
July 7, 2019
Subject Category
Man/System Technology And Life Support
Report/Patent Number
JSC-E-DAA-TN68200
Meeting Information
Meeting: International Conference on Environmental Systems
Location: Boston, MA
Country: United States
Start Date: July 7, 2019
End Date: July 11, 2019
Sponsors: International Conference On Environmental Systems, Inc.
Funding Number(s)
CONTRACT_GRANT: NNJ06TA25C
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
Safety
Injury
Helmet
NASA
Biomechanics
OCSS
NASA
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